FR2523072B1 - - Google Patents
Info
- Publication number
- FR2523072B1 FR2523072B1 FR8203961A FR8203961A FR2523072B1 FR 2523072 B1 FR2523072 B1 FR 2523072B1 FR 8203961 A FR8203961 A FR 8203961A FR 8203961 A FR8203961 A FR 8203961A FR 2523072 B1 FR2523072 B1 FR 2523072B1
- Authority
- FR
- France
- Prior art keywords
- wing
- fuselage
- zone
- attachment
- wings
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/06—Aircraft not otherwise provided for having disc- or ring-shaped wings
- B64C39/068—Aircraft not otherwise provided for having disc- or ring-shaped wings having multiple wings joined at the tips
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
- Tires In General (AREA)
- Laminated Bodies (AREA)
- Manipulator (AREA)
- Types And Forms Of Lifts (AREA)
Abstract
The invention relates to an aircraft provided on either side of its fuselage with at least one lift structure constituted by at least two wings whose distal ends are connected either to each other or to at least one wing element, each structure forming in front elevation of said fuselage a closed polygon, and comprising an upper wing and a lower wing, the zone of attachment of the latter on the fuselage possibly being offset in the direction of the streamline flow with respect to the zone of attachment of the upper wing. According to the invention, each of the wings is made so that the values of the moment of inertia and of the lift, both varying as a function of the longitudinal distance, each take a maximum value at a zone of the wing other than the root. The invention is more particularly applicable to aircraft with multiple wing elements.
Priority Applications (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8203961A FR2523072A1 (en) | 1982-03-09 | 1982-03-09 | AIRCRAFT PROVIDED WITH A MULTIPLE OVERLAPPING SUSPENSION STRUCTURE |
US06/471,059 US4541593A (en) | 1982-03-09 | 1983-03-01 | Aircraft providing with a lift structure incorporating multiple superposed wings |
DE8383400469T DE3367571D1 (en) | 1982-03-09 | 1983-03-07 | Aircraft provided with a superposed multiple-wing lift structure |
EP83400469A EP0088696B1 (en) | 1982-03-09 | 1983-03-07 | Aircraft provided with a superposed multiple-wing lift structure |
AT83400469T ATE23500T1 (en) | 1982-03-09 | 1983-03-07 | AIRCRAFT EQUIPPED WITH A MULTI-DECKER LIFT STRUCTURE. |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8203961A FR2523072A1 (en) | 1982-03-09 | 1982-03-09 | AIRCRAFT PROVIDED WITH A MULTIPLE OVERLAPPING SUSPENSION STRUCTURE |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2523072A1 FR2523072A1 (en) | 1983-09-16 |
FR2523072B1 true FR2523072B1 (en) | 1984-11-09 |
Family
ID=9271801
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR8203961A Granted FR2523072A1 (en) | 1982-03-09 | 1982-03-09 | AIRCRAFT PROVIDED WITH A MULTIPLE OVERLAPPING SUSPENSION STRUCTURE |
Country Status (5)
Country | Link |
---|---|
US (1) | US4541593A (en) |
EP (1) | EP0088696B1 (en) |
AT (1) | ATE23500T1 (en) |
DE (1) | DE3367571D1 (en) |
FR (1) | FR2523072A1 (en) |
Families Citing this family (45)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2557065A1 (en) * | 1983-12-22 | 1985-06-28 | Nguyen Manh Khanh | Aerodyne with polyhedral wing unit |
DE3710703A1 (en) * | 1987-03-31 | 1988-10-13 | Manfred Uellenberg | Wing system for fixed-wing aircraft having two lift-generating wings |
DE3737990A1 (en) * | 1987-11-09 | 1988-06-09 | Dieter Schulz | ULTRA-LIGHT COMPOSITE AIRCRAFT |
US5114097A (en) * | 1991-04-29 | 1992-05-19 | Williams International Corporation | Aircraft |
RU2001842C1 (en) * | 1991-11-27 | 1993-10-30 | Владимир Сергеевич Егер | Light multipurpose aircraft |
EP0619224A4 (en) * | 1991-11-27 | 1995-06-14 | Vladimir Sergeevich Eger | Light aeroplane. |
DE69430198T2 (en) * | 1994-12-16 | 2003-07-10 | Aldo Frediani | Wide-bodied aircraft |
WO1996036533A1 (en) * | 1995-05-15 | 1996-11-21 | Tovarischestvo S Ogranichennoi Otvetstvennostju 'arkhar' | Aircraft with equalising controls |
US5839691A (en) | 1996-05-22 | 1998-11-24 | Lariviere; Jean Soulez | Vertical takeoff and landing aircraft |
US6098923A (en) * | 1998-03-13 | 2000-08-08 | Lockheed Martin Corporation | Aircraft structure to improve directional stability |
US6474604B1 (en) * | 1999-04-12 | 2002-11-05 | Jerry E. Carlow | Mobius-like joining structure for fluid dynamic foils |
FR2806698B1 (en) | 2000-11-06 | 2002-08-02 | Lucien Cabrol | WING STRUCTURE AND MOBILE MACHINERY, ESPECIALLY FLYING MACHINES, COMPRISING SUCH A WING STRUCTURE |
WO2002046038A2 (en) | 2000-12-08 | 2002-06-13 | Lockheed Martin Corporation | Joined wing supersonic aircraft |
US6749153B1 (en) * | 2002-12-04 | 2004-06-15 | The Boeing Company | Survivable and reusable launch vehicle |
US20050116087A1 (en) * | 2003-06-11 | 2005-06-02 | Page John S.Jr. | Aircraft converts drag to lift |
US7100867B2 (en) * | 2004-02-09 | 2006-09-05 | Houck Ii Ronald G | Lifting foil |
US7131611B2 (en) * | 2004-07-30 | 2006-11-07 | Saint Louis University | Device and method of control of fixed and variable geometry rhomboid wings |
US20060060696A1 (en) * | 2004-08-26 | 2006-03-23 | Cordy Clifford B Jr | Link between the wing and canard for flutter reduction |
US7841559B1 (en) | 2006-02-16 | 2010-11-30 | Mbda Incorporated | Aerial vehicle with variable aspect ratio deployable wings |
US7644892B1 (en) | 2006-07-06 | 2010-01-12 | Alford Jr Lionel D | Blended winglet |
US7900876B2 (en) * | 2007-08-09 | 2011-03-08 | The Boeing Company | Wingtip feathers, including forward swept feathers, and associated aircraft systems and methods |
US20090084904A1 (en) * | 2007-10-02 | 2009-04-02 | The Boeing Company | Wingtip Feathers, Including Paired, Fixed Feathers, and Associated Systems and Methods |
US8128035B2 (en) * | 2008-04-15 | 2012-03-06 | The Boeing Company | Winglets with recessed surfaces, and associated systems and methods |
US9302766B2 (en) * | 2008-06-20 | 2016-04-05 | Aviation Partners, Inc. | Split blended winglet |
DK2905222T3 (en) | 2008-06-20 | 2020-01-02 | Aviation Partners Inc | CRUMPING FINGER TIP |
US8387912B2 (en) * | 2008-08-04 | 2013-03-05 | II Ronald G. Houck | Lifting foil |
EP3789725A1 (en) | 2009-02-02 | 2021-03-10 | Aerovironment | Multimode unmanned aerial vehicle |
FR2941915B1 (en) * | 2009-02-12 | 2013-05-10 | Airbus France | AIRCRAFT WITH TWO PAIRS OF WINGS |
CN106800085B (en) | 2009-09-09 | 2020-08-18 | 威罗门飞行公司 | Elevon control system |
CA2789722C (en) | 2009-09-09 | 2018-08-28 | Aerovironment, Inc. | Systems and devices for remotely operated unmanned aerial vehicle report-suppressing launcher with portable rf transparent launch tube |
GB201011843D0 (en) * | 2010-07-14 | 2010-09-01 | Airbus Operations Ltd | Wing tip device |
FR2962971B1 (en) * | 2010-07-20 | 2013-07-12 | Airbus Operations Sas | DEVICE AND METHOD FOR LATERAL STABILIZATION OF AN AIRCRAFT |
FI126015B (en) * | 2011-03-21 | 2016-05-31 | Flynano Ltd Oy | flight Unit |
EP3650337B1 (en) | 2011-06-09 | 2020-11-25 | Aviation Partners, Inc. | The split blended winglet |
US8936219B2 (en) | 2012-03-30 | 2015-01-20 | The Boeing Company | Performance-enhancing winglet system and method |
US9079663B2 (en) * | 2013-02-27 | 2015-07-14 | Northrop Grumman Systems Corporation | Canard-locked oblique wing aircraft |
FR3006665B1 (en) | 2013-06-05 | 2016-11-18 | Abraxa Sa | AILAR STRUCTURE AND MOBILE DEVICES, IN PARTICULAR FLYING GEAR, COMPRISING SUCH AILAR STRUCTURE. |
US10562613B2 (en) * | 2013-12-04 | 2020-02-18 | Tamarack Aerospace Group, Inc. | Adjustable lift modification wingtip |
GB2524824B (en) * | 2014-04-04 | 2020-06-24 | Airbus Operations Ltd | An aircraft wing with a wing tip device and a strut |
US9511850B2 (en) | 2014-04-12 | 2016-12-06 | The Boeing Company | Wing tip device for an aircraft wing |
DE102015111032A1 (en) * | 2015-07-08 | 2017-01-12 | Technische Universität Dresden | Wing assembly in boxwing configuration |
EP3269635A1 (en) * | 2016-07-12 | 2018-01-17 | The Aircraft Performance Company UG | Airplane wing |
EP3511243B1 (en) * | 2018-01-15 | 2021-12-29 | The Aircraft Performance Company GmbH | Airplane wing |
EP3837164A1 (en) | 2018-08-19 | 2021-06-23 | Hernadi, Andras | Methods for improvements of the closed wing aircraft concept and corresponding aircraft configurations |
KR102130467B1 (en) * | 2018-12-14 | 2020-07-07 | 에어버스 헬리콥터스 도이칠란트 게엠베하 | Braced wing aircraft |
Family Cites Families (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB157271A (en) * | 1919-10-27 | 1922-04-10 | Zeppelin Werke G M B H | Supporting plane for flying machines |
US1558958A (en) * | 1923-05-14 | 1925-10-27 | Percy J Williams | Airplane construction |
US1549079A (en) * | 1924-11-17 | 1925-08-11 | Themselves And The Gloucesters | Biplane wing for aircraft |
DE525387C (en) * | 1927-06-30 | 1931-10-06 | Jacob Emil Noeggerath Dr Ing | Airplane with elastically suspended wings that can move about longitudinal axes |
US1650954A (en) * | 1927-07-09 | 1927-11-29 | James M Miller | Airplane |
US1802283A (en) * | 1928-02-24 | 1931-04-21 | Simmonds Oliver Edwin | Aeroplane wing |
FR736876A (en) * | 1932-05-10 | 1932-11-30 | Aerial sailboat | |
US2075787A (en) * | 1932-11-22 | 1937-04-06 | Adams Herbert Luther | Tiltable wing |
FR1397402A (en) * | 1964-03-18 | 1965-04-30 | Improvements to airplanes, spacecraft or vehicles | |
US3695557A (en) * | 1970-08-28 | 1972-10-03 | Curtis H Pitts | Biplane construction |
US3834654A (en) * | 1973-03-19 | 1974-09-10 | Lockheed Aircraft Corp | Boxplane wing and aircraft |
US4053125A (en) * | 1973-08-30 | 1977-10-11 | Alexander Ratony | Staggered channel wing-type aircraft |
US3985317A (en) * | 1975-01-31 | 1976-10-12 | Alexander Geraci | Short coupled airplane with variable wing lift |
DE2555718C3 (en) * | 1975-12-11 | 1982-12-30 | Dornier Gmbh, 7990 Friedrichshafen | Airplane with two backward-swept wings arranged one above the other |
US4146199A (en) * | 1977-08-01 | 1979-03-27 | Phoenixbird, Inc. | Multi-winged lifting body aircraft |
US4365773A (en) * | 1979-04-11 | 1982-12-28 | Julian Wolkovitch | Joined wing aircraft |
DE2944743C2 (en) * | 1979-11-06 | 1982-07-29 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Airfoil for a high-speed aircraft |
-
1982
- 1982-03-09 FR FR8203961A patent/FR2523072A1/en active Granted
-
1983
- 1983-03-01 US US06/471,059 patent/US4541593A/en not_active Expired - Fee Related
- 1983-03-07 AT AT83400469T patent/ATE23500T1/en not_active IP Right Cessation
- 1983-03-07 DE DE8383400469T patent/DE3367571D1/en not_active Expired
- 1983-03-07 EP EP83400469A patent/EP0088696B1/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
FR2523072A1 (en) | 1983-09-16 |
EP0088696A1 (en) | 1983-09-14 |
ATE23500T1 (en) | 1986-11-15 |
US4541593A (en) | 1985-09-17 |
DE3367571D1 (en) | 1987-01-02 |
EP0088696B1 (en) | 1986-11-12 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |